N269UE1990 Embraer EMB-120RT
This N-number isn't registered right now. Below is its last known registration, canceled Jul 29, 2004.
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply34 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- International Airline Support Group INC
- Owner type
- Corporation
- City, state
- Atlanta, GA
- Certificate issued
- Jul 14, 1999
- Canceled
- Jul 29, 2004
- Airworthiness
- Standard · Transport
- Airworthiness date
- Jul 28, 1990
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Embraer
- Model
- EMB-120RT
- Year
- 1990
- Serial number
- 120.194
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 32
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A2A233
Engine
- Make and model
- P&W Canada Pw118
- Type
- Turbo-prop
- Power
- 1800 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 1999 – 2004International Airline Support Group INCAtlanta, GA
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (6)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2025-02-09 | Fuselage | Mar 18, 2025 | Airframe (EMB-120RT) |
| 2017-10-04 | Landing Gear | Jun 29, 2017 | Airframe (EMB-120RT) |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (PW118)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs. |
| 2008-04-18 R1 | EMBRAER Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes | Nov 16, 2009 | Airframe (EMB-120RT) |
| 2007-26-21 | EMBRAER Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes | Feb 20, 2008 | Airframe (EMB-120RT) |
Show all 6 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2003-21-03 | Pratt & Whitney Canada Models PW118, PW120, PW120A, and PW121 Turboprop Engines | Nov 20, 2003 | Engine (PW118) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (34)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Flight controls · actuator · malfunctionedJan 8, 2003
FLAP LIGHT ON MAP PANEL ASSOCIATED WITH ADVANCED SWS AND CONTROL FAULT ON OVERHEAD. REPLACED LEFT NACELLE FLAP ACTUATOR PER MM 27-50-00. CYCLED FLAPS SEVERAL TIMES. ALL CHECKS GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · control unit · malfunctionedNov 22, 2002
FLAPS HAD RT INBOARD FLAP ASYMMETRY WHEN SET FOR LANDING AND FAILED TO RETRACT AFTER LANDING (RT AND LT INBOARD). RE-RACKED FLAP CONTROL UNIT. PERFORMED FUNCTIONAL CHECK OF FLAP SYSTEM. CYCLED FLAPS SEVERAL TIMES. NO DISCREPANCIES NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · terminal · brokenNov 21, 2002
DURING THE TAKEOFF RUN THE NR 1 GEN OFF BUS LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED. ATTEMPTED RESET PER QRH WITH NO SUCCESS. FOUND BROKEN WIRE ON NR 1 GENERATOR. REPLACED WIRE EYELET WITH SERVICEABLE UNIT AND CONNECTED TO NR 1 GENERATOR. RAN RT ENGINE, APPLIED LOAD TO NR 1 GENERATOR AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Flight controls · control unit · malfunctionedNov 14, 2002
CONTROL FAULT ON INBOARD FLAPS AFTER TRYING TO RAISE FLAPS. REMOVED AND REPLACED FLAP CONTROL UNIT. FLAPS FUNCTIONAL CHECK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · actuator · malfunctionedOct 29, 2002
AFTER FLAP RETRACTION ON LANDING, THE INBOARD PAIR OF FLAPS REMAINED AT 25 DEGREES. THERE WERE NO CONTROL FAULTS OR DISAGREEMENT WARNINGS. AFTER RESETTING THE SYSTEM, THE FLAPS RETRACTED. REPLACED LEFT INBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPS CHECK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Indicating and recording systems · warning system · false activationAug 6, 2002
ON TAKEOFF GOT TRIPLE CHIME EEC WARNING. ABORTED TAKEOFF. SUSPECT LEFT EEC THE CULPRIT, LOWER NP THAN RT ON FFOD. INSPECTED CANNON PLUGS AND WIRING FOR CHAFING ON LT ENGINE EEC. RAN ENGINE FOR TRIM CHECK AND TAXIED AIRCRAFT. COULD NOT DUPLICATE. OPS CHECK GOOD. NO DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Pneumatic · duct · leakingJun 25, 2002
AT ABOUT 50 KTS ON TAKEOFF ROLL, TRIPLE CHIME DUCT LEAK RED LIGHT ON MAP AND DUCT LEAKAGE ON LEFT SIDE OVERHEAD. ABORTED TAKEOFF. LIGHTS REMAINED ON FOR ONLY 10-15 SECONDS, THEN WENT OUT. INSTALLED SERVICEABLE LEFT WING BLEED LINE. OPS CHECK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · actuator · malfunctionedMay 25, 2002
LEFT OUTBOARD FLAP DEPLOYED APPROXIMATELY 3 DEGREES (UNCOMMANDED) WHILE FLAP HANDLE IS IN ZERO POSITION. ANALOG INDICATOR SHOWS ZERO DEGREES. FLAP ON MAP ILLUMINATED, ASYMMETRY ON FLAP PANEL INDICATOR ILLUMINATED. REPLACED LEFT OUTBOARD FLAP ACTUATOR PER EMB 120 27-50-00. OPS CHECKS GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · eec · malfunctionedMay 20, 2002
ABORTED TAKEOFF IN FAT DUE TO LEFT EEC FAILURE. RAN NR 1 ENGINE IAW 71-00-00. RAN WITHIN PARAMETERS. OPS CHECKS GOOD AT THIS TIME. NO OTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · connector · dirtyApr 22, 2002
WHILE IN POSITION FOR TAKEOFF, RECEIVED AN AURAL WARNING ENGINE CONTROLS AND MOMENTARY RED EEC LIGHT. CLEANED P1 CONNECTOR OF LEFT AND RIGHT EEC'S. PERFORMED ENGINE RUNS. NO DISCREPANCIES FOUND.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 34 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026